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typo in AeroDyn input file comments #182

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Aug 10, 2022
Merged

typo in AeroDyn input file comments #182

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4 changes: 2 additions & 2 deletions weis/aeroelasticse/FAST_writer.py
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Original file line number Diff line number Diff line change
Expand Up @@ -738,7 +738,7 @@ def write_AeroDyn15(self):
f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SpdSound'], 'SpdSound', '- Speed of sound (m/s)\n'))
f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['Patm'], 'Patm', '- Atmospheric pressure (Pa) [used only when CavitCheck=True]\n'))
f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['Pvap'], 'Pvap', '- Vapour pressure of fluid (Pa) [used only when CavitCheck=True]\n'))
f.write('====== Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]\n')
f.write('====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0 or 3]\n')
f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SkewMod'], 'SkewMod', '- Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]\n'))
f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['SkewModFactor'], 'SkewModFactor', '- Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0 or 3]\n'))
f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['TipLoss'], 'TipLoss', '- Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3]\n'))
Expand All @@ -748,7 +748,7 @@ def write_AeroDyn15(self):
f.write('{!s:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['TIDrag'], 'TIDrag', '- Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]\n'))
f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['IndToler'], 'IndToler', '- Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]\n'))
f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['MaxIter'], 'MaxIter', '- Maximum number of iteration steps (-) [unused when WakeMod=0]\n'))
f.write('====== Dynamic Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]\n')
f.write('====== Dynamic Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=2]\n')
f.write('{:<22d} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['DBEMT_Mod'], 'DBEMT_Mod', '- Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]\n'))
f.write('{:<22} {:<11} {:}'.format(self.fst_vt['AeroDyn15']['tau1_const'], 'tau1_const', '- Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]\n'))
f.write('====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when WakeMod=3]\n')
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